Effects of airfoil shape, thickness, camber, and angle of attack on calculated transonic unsteady airloads /

Effects of airfoil shape, thickness, camber, and angle of attack on calculated transonic unsteady airloads /

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Bibliographic Details
Author / Creator:	Batina, John T.
Imprint:	Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985.
Description:	1 volume.
Language:	English
Series:	NASA technical memorandum ; 86320 NASA technical memorandum ; 86320.
Subject:	Aerofoils. Camber (Aerofoils) Unsteady flow (Aerodynamics) Aerodynamics, Transonic. Aerodynamic load.
Format:	E-Resource Microform U.S. Federal Government Document Book
URL for this record:	http://pi.lib.uchicago.edu/1001/cat/bib/7243330

Hidden Bibliographic Details
Other authors / contributors:	United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Notes:	Available via Internet from the NTRS web site. Address as of 07/08/08: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19850010648%5F1985010648.pdf ; current access is available via PURL.
GPO item no.:	0830-D (MF) 0830-D (online)
Govt.docs classification:	NAS 1.15:86320

Description
Physical Description:	1 volume.
Format:	Available via Internet from the NTRS web site. Address as of 07/08/08: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19850010648%5F1985010648.pdf ; current access is available via PURL.